Development of a three dimensional visualization tool for spacecraft attitude and orbital dynamics using telemetry data

Small satellite builders frequently encounter many different types of problems in testing different satellite subsystems at ground based laboratories. Full-scale testing can only be performed in orbit with actual flight systems, where critical errors sometimes cannot be resolved. Unlike huge budget...

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Main Author: Abdelrahman, Mohammad
Format: Monograph
Language:English
Published: s.n 2012
Subjects:
Online Access:http://irep.iium.edu.my/33698/
http://irep.iium.edu.my/33698/1/EDW_A_11-193-0984.pdf
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author Abdelrahman, Mohammad
author_facet Abdelrahman, Mohammad
author_sort Abdelrahman, Mohammad
building IIUM Repository
collection Online Access
description Small satellite builders frequently encounter many different types of problems in testing different satellite subsystems at ground based laboratories. Full-scale testing can only be performed in orbit with actual flight systems, where critical errors sometimes cannot be resolved. Unlike huge budget missions, small satellite programs are supposed to have severe limitation in time, financial, and manpower resources. The future target of the project is to design, build, and test the mission software programs for spacecraft systems i.e., the ground control station computer and the on board computer.
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format Monograph
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institution International Islamic University Malaysia
institution_category Local University
language English
last_indexed 2025-11-14T15:39:21Z
publishDate 2012
publisher s.n
recordtype eprints
repository_type Digital Repository
spelling iium-336982014-01-22T00:28:07Z http://irep.iium.edu.my/33698/ Development of a three dimensional visualization tool for spacecraft attitude and orbital dynamics using telemetry data Abdelrahman, Mohammad TJ210.2 Mechanical devices and figures. Automata. Ingenious mechanism. Robots (General) Small satellite builders frequently encounter many different types of problems in testing different satellite subsystems at ground based laboratories. Full-scale testing can only be performed in orbit with actual flight systems, where critical errors sometimes cannot be resolved. Unlike huge budget missions, small satellite programs are supposed to have severe limitation in time, financial, and manpower resources. The future target of the project is to design, build, and test the mission software programs for spacecraft systems i.e., the ground control station computer and the on board computer. s.n 2012-10-31 Monograph NonPeerReviewed application/pdf en http://irep.iium.edu.my/33698/1/EDW_A_11-193-0984.pdf Abdelrahman, Mohammad (2012) Development of a three dimensional visualization tool for spacecraft attitude and orbital dynamics using telemetry data. Research Report. s.n. (Unpublished) EDW A11-193-0984
spellingShingle TJ210.2 Mechanical devices and figures. Automata. Ingenious mechanism. Robots (General)
Abdelrahman, Mohammad
Development of a three dimensional visualization tool for spacecraft attitude and orbital dynamics using telemetry data
title Development of a three dimensional visualization tool for spacecraft attitude and orbital dynamics using telemetry data
title_full Development of a three dimensional visualization tool for spacecraft attitude and orbital dynamics using telemetry data
title_fullStr Development of a three dimensional visualization tool for spacecraft attitude and orbital dynamics using telemetry data
title_full_unstemmed Development of a three dimensional visualization tool for spacecraft attitude and orbital dynamics using telemetry data
title_short Development of a three dimensional visualization tool for spacecraft attitude and orbital dynamics using telemetry data
title_sort development of a three dimensional visualization tool for spacecraft attitude and orbital dynamics using telemetry data
topic TJ210.2 Mechanical devices and figures. Automata. Ingenious mechanism. Robots (General)
url http://irep.iium.edu.my/33698/
http://irep.iium.edu.my/33698/
http://irep.iium.edu.my/33698/1/EDW_A_11-193-0984.pdf